CN205049547U - Air detection device with system of taking photo by plane - Google Patents
Air detection device with system of taking photo by plane Download PDFInfo
- Publication number
- CN205049547U CN205049547U CN201520634659.2U CN201520634659U CN205049547U CN 205049547 U CN205049547 U CN 205049547U CN 201520634659 U CN201520634659 U CN 201520634659U CN 205049547 U CN205049547 U CN 205049547U
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- China
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- air
- floating drum
- taking photo
- fuselage
- airduct
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Abstract
The utility model provides an air detection device with system of taking photo by plane, including fuselage, tail, frame and screw, the fuselage both sides are provided with the flotation pontoon, are provided with air intake and air outlet on the flotation pontoon, are provided with the PM2.5 detector in the flotation pontoon, install video capture device in the frame, are provided with GPS clock control module, PLC controller and wireless communication module in the fuselage, and GPS clock control module's output and PLC controller input end are connected, PLC controller output hold and PM2.5 detector control end, video capture device control end and wireless communication module connect, the utility model discloses a be provided with PM2.5 and detect sensor, harmful gas detection sensor and GPS clock control module on the aircraft, gather aerial monitoring data based on GPS reference clock to adopt wireless communication module to carry out data transmission through wireless network, at the acquireing in real time in succession of data, real -time transmission with can carry out the haze early warning based on the data result.
Description
Technical field
The utility model belongs to for coordinating with aircraft or installing to the equipment on aircraft; Flying suit; Parachute; The configuration of propulsion system or propulsion gearing or the technical field of installation, specifically relate to a kind of air detecting device with the system of taking photo by plane.
Background technology
Haze, also the dust in gray haze (mist and clouds in the twilight) air is claimed, sulfuric acid, nitric acid, the particles such as organic hydrocarbon compounds also can make air muddy, the visual field is fuzzy and cause visibility deterioration, if when horizontal visibility is less than ten thousand metres, the obstruction to vision that the aerosol systems that this non-water becomes thing to form causes is called haze (Haze) or gray haze (Dust-haze), Hong Kong Observatory claims mist and clouds in the twilight (Haze), when the difference of haze and mist is haze occurs, relative humidity is little, and the relative humidity in mist is saturated (when existing if any a large amount of nucleus of condensation, relative humidity not necessarily reach 100% just may occur saturated), the fuzzy visibility deterioration caused in the muddy visual field of air when general relative humidity is less than 80% is that haze causes, the fuzzy visibility deterioration caused in the muddy visual field of air when relative humidity is greater than 90% is that mist causes, the fuzzy visibility deterioration caused in the muddy visual field of air when relative humidity is between 80 ~ 90% is that the potpourri of haze and mist causes jointly, but its principal ingredient is haze, the Thickness Ratio of haze is thicker, 1 ~ 3 km can be reached, haze and mist, cloud is different, and there is no obvious border between clear sky district, the distribution of haze particle is more even, and the yardstick of gray haze particle is smaller, from 0.001 micron to 10 microns, mean diameter is greatly about 1 ~ 2 microns, be invisible to the naked eye the aerial particle floated.Due to molecular hazes of grain such as dust, sulfuric acid, nitric acid, the longer light ratio of its scattering wavelength is more, and thus haze seems in yellow or orange grey, existing haze early warning shows hysteresis quality, be all start to detect after haze is formed, there is no the function predicted.
Summary of the invention
In view of this, the purpose of this utility model is to provide a kind of air detecting device with the system of taking photo by plane, should with the air detecting device of the system of taking photo by plane by being provided with PM2.5 detecting sensor, harmful gas detecting sensor and gps clock control module on board the aircraft, based on the aerial Monitoring Data of GPS reference clock collection, and adopt wireless communication module to carry out data transmission by wireless network, data continuous Real-time Obtaining, instantaneous transmission and can haze early warning be carried out based on data result.
In order to solve the problems of the technologies described above, a kind of air detecting device with the system of taking photo by plane of the utility model, comprise unmanned vehicle, described unmanned vehicle comprises fuselage, tail, be arranged on the frame below fuselage and the screw propeller being arranged on body upper, described fuselage both sides are provided with floating drum, described floating drum is provided with air inlet, air outlet and the airduct be connected between air inlet and air outlet, PM2.5 detector is provided with in described floating drum, described frame is provided with video acquisition device, gps clock control module is provided with in described fuselage, PLC and wireless communication module, the output terminal of described gps clock control module is connected with PLC input end, described PLC output terminal and described PM2.5 detector control end, video acquisition device control end is connected with wireless communication module.
Further, described frame is also provided with and is no less than 1 sensor, described sensor is used for detecting CO, H respectively
2s, SO
2, NO
2, NO, Cl
2, HCN, HN
3, PH
3, ClO
2, one or more harmful gases in HCl, VOC.
Further, described airduct is arranged on floating drum center, the valve for closing airduct is provided with in described airduct, the inwall that described airduct is positioned at valve nose is provided with fresh air inlet, described airduct inwall is provided with between floating drum outer wall the air channel being connected fresh air inlet, the end in described air channel is connected with air outlet opening, and described PM2.5 detector is arranged in air channel.
Further, described tail place is provided with pusher.
Further, described floating drum is set to pyramidal structure.
Further, described floating drum is made up of glass-reinforced plastic material.
The beneficial effects of the utility model are:
The utility model passes through to be provided with PM2.5 detecting sensor, harmful gas detecting sensor and gps clock control module on board the aircraft with the air detecting device of the system of taking photo by plane, based on the aerial Monitoring Data of GPS reference clock collection, and adopt wireless communication module to carry out data transmission by wireless network, data continuous Real-time Obtaining, instantaneous transmission and can haze early warning be carried out based on data result.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model with the air detecting device of the system of taking photo by plane;
Fig. 2 is the structural representation of floating drum on the utility model aircraft.
Reference numeral: 1-fuselage; 2-screw propeller; 3-tail; 4-frame; 5-floating drum; 6-air port; 7-air outlet; 8-airduct; 9-air channel; 10-PM2.5 detector; 11-valve; 12-fresh air inlet; 13-video acquisition device; 14-sensor; 15-PLC controller; 16-GPS clock control module; 17-wireless communication module.
Embodiment
Below in conjunction with the drawings and specific embodiments, utility model is described in further detail.
Be illustrated in figure 1 the structural representation of the utility model with the air detecting device of the system of taking photo by plane, be illustrated in figure 2 the structural representation of floating drum on the utility model aircraft, a kind of air detecting device with the system of taking photo by plane of the utility model, comprise unmanned vehicle, described unmanned vehicle comprises fuselage 1, tail 3, the screw propeller 2 being arranged on the frame 4 below fuselage 1 and being arranged on above fuselage 1, described fuselage 1 both sides are provided with floating drum 5, described floating drum 5 is provided with air inlet 6, air outlet 7 and the airduct 8 be connected between air inlet 6 and air outlet 7, PM2.5 detector 10 is provided with in described floating drum 5, described frame 4 is provided with video acquisition device 13, gps clock control module 16 is provided with in described fuselage, PLC 15 and wireless communication module 17, the output terminal of described gps clock control module 16 is connected with PLC 15 input end, described PLC output terminal 16 and described PM2.5 detector 10 control end, video acquisition device 13 control end is connected with wireless communication module 17.
The present embodiment is by being provided with PM2.5 detecting sensor, harmful gas detecting sensor and gps clock control module on board the aircraft, based on the aerial Monitoring Data of GPS reference clock collection, and adopt wireless communication module to carry out data transmission by wireless network, data continuous Real-time Obtaining, instantaneous transmission and can haze early warning be carried out based on data result.
Further, described frame is also provided with and is no less than 1 sensor, described sensor is used for detecting CO, H respectively
2s, SO
2, NO
2, NO, Cl
2, HCN, HN
3, PH
3, ClO
2, one or more harmful gases in HCl, VOC, the present embodiment is by the content of the harmful gas such as sulfuric acid, nitric acid in monitoring air, not only can carry out prediction haze in advance, and other objectionable constituent of air can be detected, the healthy and safe and weather environmental improvement improving people provides foundation.
Further, preferred described airduct 8 is arranged on floating drum 5 center, the valve 11 for closing airduct 8 is provided with in described airduct 8, the inwall that described airduct 8 is positioned at valve 11 front end is provided with fresh air inlet 12, described airduct 8 inwall is provided with between floating drum 5 outer wall the air channel 9 being connected fresh air inlet 12, the end in described air channel 9 is connected with air outlet opening, described PM2.5 detector 10 is arranged in air channel 9, the preferred air outlet opening of the present embodiment is distributed on the surrounding of air outlet, this enforcement is by liking at all-rounder flying up and down and telling in flight course, open valve 11, air is circulated by airduct, the resistance of air can be reduced, do not carry out the quality detecting air, its reason is that now the data accuracy that detects of PM2.5 detector 10 pairs of air is poor, time aloft slowly flight or stopping are in fashion, valve-off 11, air is by fresh air inlet 12, enter air channel, discharge from air channel air outlet opening, now wind speed is in nature gustiness, be conducive to PM2.5 detector 10 pairs of air to detect, the air quality data accuracy of this detection is good, be conducive to the accuracy rate improving haze prediction.
Further, described tail 3 place is provided with pusher, and this structure is conducive to advance and the flight of all-rounder.
Further, preferred described floating drum 5 is set to pyramidal structure, and air intake opening end is arranged on the little one end of floating drum 5 diameter, and this structure is conducive to, in all-rounder is in fashion, reducing windage.
Further, preferred described floating drum 5 is made up of glass-reinforced plastic material, and this structure is conducive to, when reducing floating drum 5 weight, improving the intensity of floating drum 5.
What finally illustrate is, above embodiment is only in order to illustrate the technical solution of the utility model and unrestricted, although be described in detail the utility model with reference to preferred embodiment, those of ordinary skill in the art is to be understood that, can modify to the technical solution of the utility model or equivalent replacement, and not departing from aim and the scope of technical solutions of the utility model, it all should be encompassed in the middle of right of the present utility model.
Claims (6)
1. the air detecting device with the system of taking photo by plane, comprise unmanned vehicle, described unmanned vehicle comprises fuselage, tail, be arranged on the frame below fuselage and the screw propeller being arranged on body upper, it is characterized in that: described fuselage both sides are provided with floating drum, described floating drum is provided with air inlet, air outlet and the airduct be connected between air inlet and air outlet, PM2.5 detector is provided with in described floating drum, described frame is provided with video acquisition device, gps clock control module is provided with in described fuselage, PLC and wireless communication module, the output terminal of described gps clock control module is connected with PLC input end, described PLC output terminal and described PM2.5 detector control end, video acquisition device control end is connected with wireless communication module.
2. the air detecting device with the system of taking photo by plane according to claim 1, is characterized in that: described frame is also provided with and is no less than 1 sensor, and described sensor is used for detecting CO, H respectively
2s, SO
2, NO
2, NO, Cl
2, HCN, HN
3, PH
3, ClO
2, one or more harmful gases in HCl, VOC.
3. the air detecting device with the system of taking photo by plane according to claim 1, it is characterized in that: described airduct is arranged on floating drum center, the valve for closing airduct is provided with in described airduct, the inwall that described airduct is positioned at valve nose is provided with fresh air inlet, described airduct inwall is provided with between floating drum outer wall the air channel being connected fresh air inlet, the end in described air channel is connected with air outlet opening, and described PM2.5 detector is arranged in air channel.
4. the air detecting device with the system of taking photo by plane according to claim 1, is characterized in that: described tail place is provided with pusher.
5. the air detecting device with the system of taking photo by plane according to claim 1, is characterized in that: described floating drum is set to pyramidal structure.
6. the air detecting device with the system of taking photo by plane according to claim 1, is characterized in that: described floating drum is made up of glass-reinforced plastic material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520634659.2U CN205049547U (en) | 2015-08-21 | 2015-08-21 | Air detection device with system of taking photo by plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520634659.2U CN205049547U (en) | 2015-08-21 | 2015-08-21 | Air detection device with system of taking photo by plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205049547U true CN205049547U (en) | 2016-02-24 |
Family
ID=55343116
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520634659.2U Expired - Fee Related CN205049547U (en) | 2015-08-21 | 2015-08-21 | Air detection device with system of taking photo by plane |
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| Country | Link |
|---|---|
| CN (1) | CN205049547U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106710151A (en) * | 2017-01-24 | 2017-05-24 | 柳州得实科技有限公司 | Ozone parameter monitor |
-
2015
- 2015-08-21 CN CN201520634659.2U patent/CN205049547U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106710151A (en) * | 2017-01-24 | 2017-05-24 | 柳州得实科技有限公司 | Ozone parameter monitor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160224 Termination date: 20160821 |